A Quiet Propeller for Commuter and General Aviation Aircraft Hartzell Propeller, Incorporated

Format:

Conference/Event

Author/Creator:

Harlamert, W. B., author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1974-04-02 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1974

Summary:

An aircraft propeller with five blades has been developed for application on relatively high horsepower turbine engines. This propeller is capable of absorbing high horsepower at low engine rpm to effect a low propeller noise emission.Propeller performance remains satisfactory, as its design is intended for a commuter type aircraft. Structurally, the addition of a blade has not created serious design problems. For its intended application, the five-blade best satisfies the requirement for a "quiet" propeller. It is doubtful if the addition of more blades would be desirable

Notes:

Vendor supplied data

Publisher Number:

740359

Access Restriction:

Restricted for use by site license